US4729339A - Pressure differential indicator with non-mechanical thermal lockout - Google Patents
Pressure differential indicator with non-mechanical thermal lockout Download PDFInfo
- Publication number
- US4729339A US4729339A US06/854,305 US85430586A US4729339A US 4729339 A US4729339 A US 4729339A US 85430586 A US85430586 A US 85430586A US 4729339 A US4729339 A US 4729339A
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- United States
- Prior art keywords
- reciprocable
- indicator
- reciprocable piston
- piston
- fluid system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 33
- 239000012530 fluid Substances 0.000 claims description 62
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 14
- 238000005096 rolling process Methods 0.000 claims description 13
- 238000007789 sealing Methods 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 239000000696 magnetic material Substances 0.000 claims 5
- 239000007788 liquid Substances 0.000 abstract description 27
- 230000000717 retained effect Effects 0.000 abstract description 6
- 230000006835 compression Effects 0.000 description 11
- 238000007906 compression Methods 0.000 description 11
- 230000008859 change Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- AMWRITDGCCNYAT-UHFFFAOYSA-L hydroxy(oxo)manganese;manganese Chemical compound [Mn].O[Mn]=O.O[Mn]=O AMWRITDGCCNYAT-UHFFFAOYSA-L 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000004044 response Effects 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 210000003141 lower extremity Anatomy 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L7/00—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements
- G01L7/16—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements in the form of pistons
- G01L7/166—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements in the form of pistons with mechanical transmitting or indicating means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D35/00—Filtering devices having features not specifically covered by groups B01D24/00 - B01D33/00, or for applications not specifically covered by groups B01D24/00 - B01D33/00; Auxiliary devices for filtration; Filter housing constructions
- B01D35/14—Safety devices specially adapted for filtration; Devices for indicating clogging
- B01D35/143—Filter condition indicators
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L13/00—Devices or apparatus for measuring differences of two or more fluid pressure values
- G01L13/02—Devices or apparatus for measuring differences of two or more fluid pressure values using elastically-deformable members or pistons as sensing elements
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L7/00—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements
- G01L7/16—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements in the form of pistons
- G01L7/163—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements in the form of pistons construction or mounting of pistons
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S116/00—Signals and indicators
- Y10S116/42—Oil filter
Definitions
- This invention relates to a device to indicate an unacceptable pressure differential across the filter in a liquid circuit, such as a lubricating oil circuit or an hydraulic circuit. More particularly, this invention relates to a pressure differential indicator that has a nonmechanical temperature sensitive lockout feature to prevent the device from giving an excessive pressure differential condition indication when such condition exists by virtue of the viscosity of the circulating fluid at low temperatures, as opposed to a clogged condition of the filters.
- 3,117,550 discloses a temperature sensitive pressure differential indicator in which the actuation of an indicator pin into a high pressure differential indicating position is effected by the springing of a temperature-compensating bimetallic convex disk; and U.S. Pat. No. 4,172,971 (Silverwater, et al) discloses a temperature sensitive pressure differential indicator which utilizes axially aligned magnetic elements in the actuation of the high pressure differential indicating button, with a thermostatic element to physically decouple the system at low operating temperatures to prevent a false indication of a high pressure differential at such low temperatures.
- Other prior patents which disclose the use of bimetallic temperature lockout elements in a liquid filter excessive pressure differential indicator are U.S. Pat. Nos. 3,812,816 (Juhasz); 3,386,410 (Barnes, Jr.); 3,402,690 (Willis); 3,140,690 (Siebel); and 2,942,572 (Pall).
- Prior art devices of the type described above have certain problems associated with their use, however.
- One of the problems is that they rely on mechanical interference between parts that are movable relative to one another in response to a change in temperature to perform the thermal lockout feature, and the movement of such parts relative to one another, and the loads between them when they are in mechanically interferring position relative to one another lead to wear on such parts and can lead to eventual failure of one or another of such parts or loss of reliability in their operation.
- the reliance on mechanical interference between parts that are movable relative to one another for the performance of a thermal lockout feature can lead to unreliable performance of such devices in an environment where they are subject to high frequency vibrations or shock loads of substantial magnitude.
- a differential pressure indicator for indicating a clogged condition of a filter in a liquid circulating system, such as hydraulic fluid in an hydraulic system or oil in a lubrication system.
- the differential pressure indicator of this invention incorporates a temperature sensitive feature to lockout the operation of the differential pressure indicator during times when the temperature of the circulating liquid is below a predetermined value, when an excessive differential pressure condition can result from an increased viscosity of the circulating liquid, as opposed to a clogged condition in the filter that is being monitored by the differential pressure indicator.
- the temperature sensitive lockout feature of the differential pressure indicator of the present invention results solely from the magnetic characteristics of the various elements of such indicator, one of such elements being an annular thermal ferrite element.
- This thermal ferrite element reversibly, suffers a substantial change in its magnetic properties over a very narrow temperature range, known as the Curie point, being magnetic below the Curie point and substantially less magnetic above the Curie point.
- the annular thermal ferrite element cooperates with a permanent magnetic element, an armature and a magnetic iron pole piece, to retain a spring biased indicator button element of the indicator, which carries the armature, in its closed or non-indicating position at temperatures below the Curie point, by magnetic forces that act to retain the armature in the nonindicating position, notwithstanding a differential pressure condition that would otherwise permit the spring that acts on the indicator button to bias it to its released or indicating position.
- temperatures of the thermal ferrite element above its Curie point it suffers such a loss in its magnetic characteristics that it is unable to complete the magnetic circuit that acts on the armature carried by the indicator button, thus freeing the indicator button to release, under the force of the spring that acts against it, in response to an excessive differential pressure condition.
- the thermal lockout feature of the differential pressure indicator of the present invention does not depend on a thermally sensitive mechanical interference condition between parts that are movable with respect to one another, and is thereby free from the problems of wear, failure and susceptibility to vibrations and shock loads that apply to differential pressure indicators which utilize such thermally sensitive mechanical lockout features.
- an object of the present invention to provide an indicator for indicating an excessive differential pressure condition in a circulating liquid system with an improved feature for locking out or suspending the operation of the indicator during periods of low liquid temperature.
- FIG. 1 is an elevational view, in section, of a preferred embodiment of a pressure differential indicator according to the present invention, showing the indicator in the position where it is not indicating an excessive pressure differential condition;
- FIG. 2 is an elevational view, in section, of the pressure differential indicator of FIG. 1 showing the indicator in the position where it is indicating an excessive pressure differential condition;
- FIG. 3 is an elevational view, in section, of an alternative embodiment of a pressure differential indicator according to the present invention, showing the indicator in the position where it is not indicating an excessive pressure differential condition;
- FIG. 4 is an elevational view, in section, of another alternative embodiment of a pressure differential indicator according to the present invention, showing the indicator in the position where it is not indicating an excessive pressure differential condition;
- FIG. 5 is an elevational view, in section, of yet another alternative embodiment of a pressure differential indicator according to the present invention, showing the indicator in the position where it is not indicating an excessive pressure differential condition.
- the preferred embodiment of a pressure differential indicator according to the present invention is generally indicated by reference numeral 10 in FIGS. 1 and 2.
- the pressure differential indicator 10 is actually shown at an enlarged scale, it being possible and preferred, for reasons of cost and ease of installation, to keep such pressure differential indicator 10 relatively small, for example, less than one and one-half inches (11/2 in.) in vertical height.
- the pressure differential indicator 10 includes an irregularly-shaped annular body portion 12 which has an annular flange 14 extending therefrom.
- the annular flange 14 is adapted to bear against a surface S of a member M to which the pressure differential indicator 10 is affixed, the annular body portion 12 of the pressure differential indicator 10 having an externally threaded portion 16 which is threaded into an internally threaded portion T of the member M to facilitate the affixing of the pressure differential indicator 10 to the member M.
- an O-ring seal 0 is trapped therebetween as is known in the art.
- the pressure differential indicator 10 has an annular piston 18 which is reciprocable within a bore 20 in the annular body portion 12 between a first position, which is shown in FIG. 1, and a second position which is shown in FIG. 2, the first position being above the second position in the vertical orientation of the pressure differential indicator depicted in FIGS. 1 and 2.
- the annular piston 18 has a web 22 extending thereacross at a location between the ends of the annular piston 18, and the web 22, thereby, forms an upper, upwardly facing pocket 24 and a lower, downwardly facing pocket 26 within the annular piston 18.
- the upper pocket 24 within the annular piston 18 has a permanent magnet 28 located therein, the permanent magnet 28 extending above the top of the annular piston 18 for reasons which will hereinafter be explained more fully, and the permanent magnet 28 is fixed within the upper pocket 24 of the annular piston 18 and reciprocates with the annular piston 18.
- the lower pocket 26 of the annular piston 18 traps the upper end of a compression spring 30, the compression spring 30 extending below the lower end of the annular piston 18 and being retained by an annular shoulder 32 that extends radially inwardly from a bore 34 in the member M 34 thus, the compression spring 30 serves to provide an upwardly directed biasing force on the annular piston 18, by virtue of the contact of the upper end of the compression spring 30 against the underside of the web 22 of the annular piston 18.
- a sliding seal 33 is positioned between the lower extremity of the annular body portion 12 and an annular shoulder in the housing M, to sealingly engage the annular piston 18 during sliding movement of the annular piston.
- the pressure differential indicator 10 is installed, with respect to the circulating liquid system being monitored, so that the underside of the web 22 of the annular piston 18 is exposed to a low pressure location within the circulating liquid system, for example, to the outlet or downstream side of a filter (not shown) that is used in the circulating liquid system, through an opening 36 in the member M, the opening 36 being defined by the inner periphery of the annular shoulder 32.
- the upper annular edge of the annular piston 18 is exposed to a high pressure location within the circulating liquid system, for example, to the inlet or upstream side of the filter, through a passage 38 which extends through the annular body portion 12 of the pressure differential indicator 10 and which communicates with a passage P in the member M.
- the various elements of the pressure differential indicator 10 are so calibrated that the force imposed on the annular piston 18 by the compression spring 30 will exceed the pressure differential force when the pressure differential force is less than a predetermined acceptable maximum, for example, when the filter of the associated liquid circulating system is clean and free flowing, and when this condition prevails, the annular piston will be in its first, FIG. 1 position.
- the pressure differential indicator 10 also includes a cup-shaped indicator button 40 which is shown in a non-indicating position in FIG. 1 where it is shrouded by an annular extension portion 42 of the annular body portion 12 and an annular retainer 44 that is pressed or crimped on the exterior of the annular extension portion 42.
- the annular retainer 44 has an annular flange 46 that extends radially inwardly from the upper portion thereof, and the annular flange 46 is adapted to engage a radially outwardly extending annular flange 48 at the base of the indicator button 40 to limit the travel of the indicator button 40 within the annular retainer 44.
- the indicator button 40 has a soft steel or iron disk 50 contained therein, illustrated as being positioned against the closed end 52 of the indicator button.
- the disk 50 serves as the armature in a magnetic circuit that includes the permanent magnet 28.
- a compression spring 54 has an upper end which acts on the underside of the disk 50 and a lower end which is retained by an upper shoulder 56 of the annular body portion 12, and the compression spring 54, therefore, acts to bias the indicator button from the lower, non-indicating position shown in FIG. 1 to the upper position shown in FIG. 2 where it serves as a visually detectable indication of an excessive pressure differential condition across the filter of the liquid circulating system being monitored by the pressure differential indicator 10.
- the annular piston 18 is in its upper position as shown in FIG.
- the indicator button 40 will be retained in its lower, non-indicating position, as shown in FIG. 1, by the magnetic force exerted by the permanent magnet 28 on the disk 50, the magnetic force from the permanent magnet 28 being transmitted to the disk 50 through a magnetically permeable iron pole piece 60.
- the permanent magnet 28 will be drawn away from the pole piece 60, thus reducing the magnetic forces transmitted through the pole piece 60 to the disk 50 and thereby allowing the compression spring 54 to move the indicator button 40 to its upper, indicating position.
- the locking out of the release of the indicator button 40 from its lower, non-indicating position, shown in FIG. 1, to its upper, indicating position, shown in FIG. 2, during periods of low circulating liquid temperature when the annular piston 18 can be moved to its second, FIG. 2, position as a result of an increase in the viscosity of the circulating liquid as opposed to a clogged condition of the filter being monitored, is accomplished by providing an annular, thermal ferrite ring 58 that slidably surrounds the portion of the permanent magnet 28 that extends above the upper edge of the annular piston 18 and that is in contact with the underside of the pole piece 60.
- the thermal ferrite ring 58 is formed from one of a family of thermal ferrite materials, which are, basically, ceramic type metal oxides mainly including iron oxide, manganese oxide and zinc oxide.
- the specific thermal ferrite material for any given application for a pressure differential indicator is selected based on its Curie point, the temperature above which its saturated magnetic flux density is severly reduced, it being desired that the Curie point correspond to the temperature below which the activation of the indicator button 40 by the movement of the annular piston 18 to its second, FIG. 2 position is to be prevented or locked out.
- the thermal ferrite ring 58 has substantial magnetic properties below its Curie point, so that it will impose a magnetic retention force on the disk 50 within the indicator button 40, a force that is sufficient to overcome the opposing force imposed by the compression spring 54 notwithstanding the movement of the annular piston 18 from its first, FIG. 1 position to its second, FIG. 2 position by virtue of an increase in the pressure differential force on the annular piston 18.
- the thermal ferrite ring 58 loses substantially all its magnetic properties, so that the indicator button 40 will then be free to move from its non-indicating, FIG. 1 position to its indicating, FIG. 2 position when an increase in the pressure differential across the annular piston 18 causes it to move from its first, FIG.
- Thermal ferrite materials of the type referred to herein are available for purchase from Nippon Ferrite, Ltd. of Tokyo, Japan through their distributor in the United States, Hitachi Magnetic Corp., a corporation with an office in Nashua, N.H.
- FIG. 3 illustrates an alternative embodiment of a pressure differential indicator according to the present invention, which is generally indicated by reference numeral 110. Except as is hereinafter described, the pressure differential indicator 110 of FIG. 3 is the same in construction and operation as the pressure differential indicator 10 of FIGS. 1 and 2.
- the pressure differential indicator 110 of FIG. 3 is intended for use in somewhat lower pressure differential liquid circulating systems than the pressure differential indicator 10 of FIGS. 1 and 2, and to be more responsive to the low or downstream pressure in such a lower pressure differential system, the pressure differential indicator is provided with a reciprocable annular piston 118 whose low pressure end is enlarged by providing it with a radially extending annular flange 119 to increase the force imposed on the reciprocable annular piston 118 by virtue of the increased surface area that is exposed to low system pressure.
- the lower end of the reciprocable annular piston 118 reciprocates within an end piece 134 of the pressure differential indicator 110 somewhat in the manner of the reciprocation of the lower end of the annular piston 18 within the bore 34 of the member M of the pressure differential indicator 10, except that the sealing of the reciprocable annular piston 118 the pressure differential indicator 110 is accomplished by a sliding seal 133 which is attached to the reciprocable annular piston 118 and slides with respect to the bore 134 of the member M1, whereas the sliding seal 33 of the pressure differential indicator 10 is retained between a counterbore in the member M and the annular piston 18 which slides with respect to such sliding seal 33.
- FIG. 4 illustrates another alternative embodiment of a pressure differential indicator according to the present invention, which is generally indicated by reference numeral 210. Except as is hereinafter described, the pressure differential indicator 210 of FIG. 4 is the same in construction and operation as the pressure differential indicator 10 of FIGS. 1 and 2.
- the pressure differential indicator 210 of FIG. 4 is a self-contained indicator, unlike the pressure differential indicator 10 which relies partially on the member M to contain its various elements and the pressure differential indicator is intended for use in liquid circulating systems that experience pulses in the pressure levels within the system.
- the pressure differential indicator 210 is designed for applications where it is necessary or desirable to utilize a self-contained indicator, and it is designed to temporarily insulate the low pressure side of a reciprocable annular piston 218 from the effects of such pulses in the pressure levels, to prevent the release of an indicator button 240 of the pressure differential indicator 210 solely as a result of a pulse in the pressure level, as opposed to an objectionably high stable pressure differential when it is desired to permit the release of the indicator button 240.
- the pressure differential indicator 210 is provided with an annular body portion 212 which is substantially longer than the annular body portion 12 of the pressure differential indicator 10 and which substantially encircles an end piece 234 of the pressure differential indicator 210.
- the end piece has a substantially closed end 232, with an orifice 236 therein is exposed to the low pressure side of the circulating liquid in the liquid circulating system.
- the annular body portion 212 of the pressure differential indicator 210 is provided with an annular filter 213 surrounding an annular recess 215 within the annular body portion to protect the high pressure side of the annular piston 218 from fouling or wear by virtue of any contaminants that may be present in the circulating fluid, which is in communication with the high pressure side of the annular piston 218 from the annular recess 215 through an orifice 238.
- the orifice 238 in the annular recess 215 is very small thus, insulating the high pressure side of the annular piston 218 from short duration pulses in the high pressure side of the circulating fluid.
- the differential pressure indicator 10 of the embodiment of FIGS. 1 and 2 and the differential pressure indicator 110 of the embodiment of FIG. 3 may also be provided with a high pressure side filter, similar to the filter 213 of the differential pressure indicator 210, where desired.
- FIG. 5 illustrates yet another alternative embodiment of a pressure differential indicator according to the present invention, which is indicated generally by reference numeral 310. Except as is hereinafter described the pressure differential indicator 310 of FIG. 5 is the same in construction and operation as the pressure differential indicator 10 of FIGS. 1 and 2.
- the pressure differential indicator 310 is intended for use in very low pressure differential liquid circulating systems where the frictional forces resulting from the use of a sliding seal such as the sliding seal 33 of the pressure differential indicator 10 would or could be high in relation to the pressure differential forces acting on a reciprocable piston, such as the annular piston 18 of the pressure differential indicator 10.
- the frictional forces resulting from a seal to seal the reciprocable annular piston 318 are very substantially reduced, relative to those which would result from the use of a sliding seal, such as the sliding seal 33 of the pressure differential indicator 10, by the use of a flexible rolling diaphragm 333 as the sealing element.
- the rolling diaphragm has an enlarged end 333a which is contained in an annular groove 312a of an annular body portion 312, and, further, the rolling diaphragm 333 has a second end 333b that is affixed to the low pressure end of the reciprocable annular piston 318, the rolling diaphragm 333 having a centering hole 333c that fits over a centering projection 318a that extends from the low pressure end of the reciprocable annular piston 318.
- the second end 333b of the rolling diaphragm 333 is retained in position with respect to the centering projection 318a of the reciprocable annular piston 318 by an inverted cup shaped member 319 that is provided with a centering hole 319a that fits over the centering projection 318a of the reciprocable annular piston 318.
- the rolling diaphragm 333 also has an intermediate portion 333d between the enlarged end 333a and the second end 333b, and the intermediate portion 333d has sufficient length, being draped in the form of a U, to accommodate all permissible travel of the annular piston 318.
- the interior of the intermediate portion 333d of the rolling diaphragm 333 is pressurized by fluid from the high pressure side of the reciprocable annular piston 318 by providing an annular clearance passage 312b between the exterior of the reciprocable annular piston 318 and the interior of the annular body portion 312 to reduce the sliding friction between the reciprocable annular piston 318 and the annular body portion 312 and prevent the development of partial vacuum within the intermediate portion 333d of the rolling diaphragm 333.
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- Measuring Fluid Pressure (AREA)
Abstract
Description
Claims (37)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/854,305 US4729339A (en) | 1986-04-21 | 1986-04-21 | Pressure differential indicator with non-mechanical thermal lockout |
| JP62095503A JPH0721435B2 (en) | 1986-04-21 | 1987-04-20 | Differential pressure measuring device |
| CA000535176A CA1288294C (en) | 1986-04-21 | 1987-04-21 | Pressure differential indicator with non-mechanical thermal lockout |
| GB8709409A GB2189603B (en) | 1986-04-21 | 1987-04-21 | Pressure differential indicator with non-mechanical thermal lockout |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/854,305 US4729339A (en) | 1986-04-21 | 1986-04-21 | Pressure differential indicator with non-mechanical thermal lockout |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US4729339A true US4729339A (en) | 1988-03-08 |
Family
ID=25318314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/854,305 Expired - Lifetime US4729339A (en) | 1986-04-21 | 1986-04-21 | Pressure differential indicator with non-mechanical thermal lockout |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US4729339A (en) |
| JP (1) | JPH0721435B2 (en) |
| CA (1) | CA1288294C (en) |
| GB (1) | GB2189603B (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4867095A (en) * | 1988-04-05 | 1989-09-19 | Parker Hannifin Corporation | Differential pressure indicator |
| US5237957A (en) * | 1992-07-08 | 1993-08-24 | Liucci Charles A | Pressure indicator |
| WO2003027624A1 (en) * | 2001-09-26 | 2003-04-03 | Perkinelmer, Inc. | Pressure indication device |
| US20040025691A1 (en) * | 2002-08-07 | 2004-02-12 | Andrew Corporation | Pressure equalization apparatus and methods |
| US20050284802A1 (en) * | 2004-06-23 | 2005-12-29 | Jankuski George A | Filtering device with integral filter status indicator |
| US7059194B1 (en) | 2000-03-15 | 2006-06-13 | Mid-West Instruments | Pressure fault device |
| US20150096363A1 (en) * | 2012-06-22 | 2015-04-09 | Innovar Engineering As | Pressure Sensing Device and Method for Using the Same |
| US9296467B1 (en) * | 2009-06-09 | 2016-03-29 | The Boeing Company | Pressure test door for use with a fuel tank |
| CN105540891A (en) * | 2015-12-11 | 2016-05-04 | 浙江沁园水处理科技有限公司 | Water purifier and filter core lifetime real-time monitor |
| CN107605864A (en) * | 2017-10-20 | 2018-01-19 | 新乡市华航航空液压设备有限公司 | A kind of New temperature lock structure signalling means |
| US9976456B2 (en) | 2013-01-24 | 2018-05-22 | Cummins Filtration Ip, Inc. | Virtual filter condition sensor |
| CN111198064A (en) * | 2018-11-16 | 2020-05-26 | 雅玛信过滤器株式会社 | Differential pressure detection device |
| CN114776876A (en) * | 2022-04-18 | 2022-07-22 | 陕西大唐燃气安全科技股份有限公司 | Gas pressure regulator, pressure regulator equipment |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2659141B1 (en) * | 1990-03-01 | 1994-03-25 | Lebozec Gautier | CLOGGING INDICATOR. |
| WO1991006357A1 (en) * | 1989-10-31 | 1991-05-16 | Le Bozec Et Gautier | Clogging indicator |
| CN104879347B (en) * | 2014-02-28 | 2018-04-20 | 北京谊安医疗系统股份有限公司 | The pneumatic display of magnetic force |
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| US2794100A (en) * | 1955-08-16 | 1957-05-28 | Wilhelm Baier Kg | Thermal relay |
| US3412706A (en) * | 1965-04-09 | 1968-11-26 | Bowser Inc | Differential pressure indicator |
| US3448716A (en) * | 1965-10-23 | 1969-06-10 | Commercial Filters Corp Of Cal | Magnetic pressure indicator |
| US3499415A (en) * | 1967-02-17 | 1970-03-10 | Btr Industries Ltd | Indicator devices |
| US3568625A (en) * | 1968-11-05 | 1971-03-09 | Fairfield Facility Commercial | Differential pressure indicator |
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| US4092586A (en) * | 1975-10-20 | 1978-05-30 | General Electric Company | Temperature-sensing circuit |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1143834A (en) * | 1965-04-30 | 1900-01-01 | ||
| GB1286808A (en) * | 1968-10-14 | 1972-08-23 | Btr Industries Ltd | Improvements in or relating to pressure indicating devices |
| US4426952A (en) * | 1981-02-09 | 1984-01-24 | Facet Enterprises, Inc. | Temperature compensated differential pressure indicating device |
| AU3423184A (en) * | 1984-01-12 | 1985-07-18 | Facet Enterprises Inc. | Temperature sensitive differential pressure indicating device |
-
1986
- 1986-04-21 US US06/854,305 patent/US4729339A/en not_active Expired - Lifetime
-
1987
- 1987-04-20 JP JP62095503A patent/JPH0721435B2/en not_active Expired - Fee Related
- 1987-04-21 GB GB8709409A patent/GB2189603B/en not_active Expired
- 1987-04-21 CA CA000535176A patent/CA1288294C/en not_active Expired - Lifetime
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| US2794100A (en) * | 1955-08-16 | 1957-05-28 | Wilhelm Baier Kg | Thermal relay |
| US3412706A (en) * | 1965-04-09 | 1968-11-26 | Bowser Inc | Differential pressure indicator |
| US3448716A (en) * | 1965-10-23 | 1969-06-10 | Commercial Filters Corp Of Cal | Magnetic pressure indicator |
| US3499415A (en) * | 1967-02-17 | 1970-03-10 | Btr Industries Ltd | Indicator devices |
| US3595200A (en) * | 1968-06-03 | 1971-07-27 | Carborundum Co | Differential pressure indicator |
| US3568625A (en) * | 1968-11-05 | 1971-03-09 | Fairfield Facility Commercial | Differential pressure indicator |
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| US4092586A (en) * | 1975-10-20 | 1978-05-30 | General Electric Company | Temperature-sensing circuit |
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Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4867095A (en) * | 1988-04-05 | 1989-09-19 | Parker Hannifin Corporation | Differential pressure indicator |
| US5237957A (en) * | 1992-07-08 | 1993-08-24 | Liucci Charles A | Pressure indicator |
| US7059194B1 (en) | 2000-03-15 | 2006-06-13 | Mid-West Instruments | Pressure fault device |
| WO2003027624A1 (en) * | 2001-09-26 | 2003-04-03 | Perkinelmer, Inc. | Pressure indication device |
| US20040025691A1 (en) * | 2002-08-07 | 2004-02-12 | Andrew Corporation | Pressure equalization apparatus and methods |
| US6800114B2 (en) | 2002-08-07 | 2004-10-05 | Andrew Corporation | Pressure equalization apparatus and methods |
| US20050284802A1 (en) * | 2004-06-23 | 2005-12-29 | Jankuski George A | Filtering device with integral filter status indicator |
| US9296467B1 (en) * | 2009-06-09 | 2016-03-29 | The Boeing Company | Pressure test door for use with a fuel tank |
| US20150096363A1 (en) * | 2012-06-22 | 2015-04-09 | Innovar Engineering As | Pressure Sensing Device and Method for Using the Same |
| US9422805B2 (en) * | 2012-06-22 | 2016-08-23 | Innovar Engineering As | Pressure sensing device and method for using the same |
| US9976456B2 (en) | 2013-01-24 | 2018-05-22 | Cummins Filtration Ip, Inc. | Virtual filter condition sensor |
| US10287935B2 (en) | 2013-01-24 | 2019-05-14 | Cummins Filtration Ip, Inc. | Virtual filter condition sensor |
| US10634022B2 (en) | 2013-01-24 | 2020-04-28 | Cummins Filtration Ip, Inc. | Virtual filter condition sensor |
| CN105540891A (en) * | 2015-12-11 | 2016-05-04 | 浙江沁园水处理科技有限公司 | Water purifier and filter core lifetime real-time monitor |
| CN107605864A (en) * | 2017-10-20 | 2018-01-19 | 新乡市华航航空液压设备有限公司 | A kind of New temperature lock structure signalling means |
| CN111198064A (en) * | 2018-11-16 | 2020-05-26 | 雅玛信过滤器株式会社 | Differential pressure detection device |
| CN114776876A (en) * | 2022-04-18 | 2022-07-22 | 陕西大唐燃气安全科技股份有限公司 | Gas pressure regulator, pressure regulator equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2189603B (en) | 1989-11-29 |
| GB2189603A (en) | 1987-10-28 |
| GB8709409D0 (en) | 1987-05-28 |
| JPS62257038A (en) | 1987-11-09 |
| CA1288294C (en) | 1991-09-03 |
| JPH0721435B2 (en) | 1995-03-08 |
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